j. Lessor shall use reasonable commercial efforts to provide Lessee with adequate information to transition the Aircraft to Lessee's maintenance program.



2) ENGINES AND APU:



 a. The Pratt & Whitney JT8D-200 Engines and APUshall have just completed a video borescope inspection, at Lessor's cost, in the presence of the Lessee of all accessible sections and also a maximum power assurance run in accordance with the Manufacturer's maintenance manual. The JT8D-200 Engines shall be delivered with a minimum of 3,000 hours and 2,000 cycles remaining to the first limited part.



 b. The JT8D-200 Engine shall have just completed a visual inspection of the Engine filters and magnetic chip detectors.



 c. No Engine shall be on "Watch" and each such Engine shall comply with the operations specification of Lessee without waiver or exceptions.





 


3) FUSELAGE, WINDOWS AND DOORS:






 a. Fuselage shall be free of major dents and abrasions, time limited patches and loose or pulled or missing rivets. All sheet metal and structural repairs shall be in compliance with the applicable manufacturer's structural repair manual or alternatively as approved and documented by the FAA. Repair and dent mapping shall be accomplished at the integration check prior to delivery to Lessee;



 b. Doors shall be free moving, correctly rigged and be fitted with serviceable seals.



4) WINGS AND EMPENNAGE AND ENGINE NACELLES:



 a. All leading edges and control surfaces shall be free from damage which exceeds the applicable Manufacturer's structural repair manual and applicable aircraft maintenance manual or Manufacturer's approved data and will not have any time limited repairs;



 b. All Engine nacelles shall be free of damage which exceeds the applicable Manufacturer maintenance manual limits;



 c. Wings shall be free of fuel leaks.